首页> 外国专利> PRIMARY STRUCTURE OF AN AIRCRAFT MOUNT COMPRISING AT LEAST ONE TRANSVERSE REINFORCEMENT PROVIDED WITH TWO RODS ARRANGED DIAGONALLY AND AIRCRAFT COMPRISING SUCH A PRIMARY STRUCTURE

PRIMARY STRUCTURE OF AN AIRCRAFT MOUNT COMPRISING AT LEAST ONE TRANSVERSE REINFORCEMENT PROVIDED WITH TWO RODS ARRANGED DIAGONALLY AND AIRCRAFT COMPRISING SUCH A PRIMARY STRUCTURE

机译:飞机架的主要结构包括至少一个横向钢筋,两个对角线布置,并且飞机具有这种主要结构

摘要

The subject of the invention is a primary structure of an aircraft mast which comprises: - upper and lower spars (52, 54), - right and left side panels (56, 58), - transverse reinforcements (60 ) arranged in transverse planes, each having a square or rectangular outline and at least one sole (64) against which are fixed the upper and lower side members (52, 54) as well as the right and left side panels (56, 58), - at least one of the transverse reinforcements (60) of the primary structure (50) comprising first and second connecting rods (66, 68), oriented along diagonals of the transverse reinforcement (60), as well as connecting systems connecting each of the first and second ends (66.1, 66.2, 68.1, 68.2) of the first and second connecting rods (66, 68) to the sole (64) or to one of the sole (64). The invention also relates to an aircraft comprising a such primary structure.
机译:本发明的主题是一种飞机桅杆的主要结构,其包括:-上部和下部梁(52、54),-左右侧板(56、58),-布置在横向平面中的横向加强件(60),每个具有正方形或矩形的轮廓,并具有至少一个鞋底(64),上侧和下侧构件(52、54)以及左右侧板(56、58)固定在其上-至少一个主结构(50)的横向加强件(60)包括沿横向加强件(60)的对角线定向的第一和第二连杆(66、68),以及连接第一和第二端部中的每一个的连接系统(第一和第二连杆(66、68)的66.1、66.2、68.1、68.2)连接至鞋底(64)或鞋底(64)之一。本发明还涉及一种包括这种主要结构的飞机。

著录项

  • 公开/公告号EP3699091A1

    专利类型

  • 公开/公告日2020-08-26

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号EP20200152222

  • 发明设计人 GLEIZE OLIVIER;

    申请日2020-01-16

  • 分类号B64D27/26;

  • 国家 EP

  • 入库时间 2022-08-21 11:39:56

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